CN110745230B - High-altitude balloon issuing device and method - Google Patents

High-altitude balloon issuing device and method Download PDF

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Publication number
CN110745230B
CN110745230B CN201911035874.XA CN201911035874A CN110745230B CN 110745230 B CN110745230 B CN 110745230B CN 201911035874 A CN201911035874 A CN 201911035874A CN 110745230 B CN110745230 B CN 110745230B
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dispensing
altitude balloon
support arm
folding support
altitude
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CN110745230A (en
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洪涛
程元
杜超
何超
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Hunan Aerospace Yuanwang Science & Technology Co ltd
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Hunan Aerospace Yuanwang Science & Technology Co ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/40Balloons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60PVEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
    • B60P3/00Vehicles adapted to transport, to carry or to comprise special loads or objects
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Transportation (AREA)
  • Jib Cranes (AREA)
  • Toys (AREA)

Abstract

The invention provides a high-altitude balloon issuing device and a high-altitude balloon issuing method. The high-altitude balloon dispensing device comprises a flat trolley and a plurality of dispensing components which are arranged on the periphery of the flat trolley and used for dragging and dispensing the high-altitude balloon, wherein the dispensing components can horizontally rotate and stretch along the flat trolley, and the dispensing components can simultaneously realize dispensing. Compared with the related art, the high-altitude balloon dispensing device system provided by the invention is simple in structure and controllable in maneuvering, can realize reliable dispensing operation of small and medium-sized high-altitude balloons through position adjustment of the folding support arm and the wire stripper, has the characteristics of low cost, easiness in operation and the like, can avoid severe weather environment in a short time when in dispensing preparation, and can fully utilize a dispensing window to realize rapid dispensing.

Description

High-altitude balloon issuing device and method
Technical Field
The invention relates to the technical field of aerostats, in particular to a high-altitude balloon dispensing device and a high-altitude balloon dispensing method.
Background
The aerostat is also called as a high-altitude scientific balloon, and is an unpowered aircraft which is lifted off by means of buoyancy gas and can fly at the altitude in the nearby space under the action of wind power. The high-altitude balloon has the advantages of high flying altitude, long dead time, low manufacturing cost, short preparation period, easy flexible deployment and the like, thus having great development value in civil and military fields and becoming a carrier which is driven by aircrafts such as rockets, artificial satellites and the like and performs various space science and technical researches.
As a mature type of high-altitude loading platform, the size of the high-altitude balloon is determined by the weight of the load and the height of the residence. At present, the design space height of the high altitude balloon is about 18km to 40km, but the weight of the carried load is two extreme: the system comprises a large scientific instrument with the weight of more than 500 kg and even several tons, and a communication load, a investigation load and a weather detection instrument with the weight of about several kg or more than ten kg. Therefore, the volume of the balloon designed by the former is usually up to hundreds of thousands of cubic meters, which belongs to heavy-load high-altitude balloon, while the balloon designed by the latter is mostly thousands of cubic meters, which is a medium-sized and small-sized high-altitude balloon. From the application potential, the small and medium-sized high-altitude balloon is simpler and cheaper than the heavy-duty high-altitude balloon, has wider application range, can be used in the fields of reconnaissance, communication, weather detection, pollution monitoring, urban management and the like, and has important development value.
The release process of the high-altitude balloon is influenced by the release mode and the field operation on one hand and is easily influenced by site meteorological conditions on the other hand. Currently, balloons mainly face several problems during the release process: (1) The balloon is a wind body in the ground inflation process, and can shake under the influence of wind speed and wind direction; (2) At the moment of balloon release, the load weight is large, so that the collision overload of the nacelle and the balloon is large, and the risk of damage is high; (3) The required guarantee resources are complex, including hauling and arrangement of the bag bodies and equipment before distribution, the ground inflation process, the number of personnel required by command operation and the requirement of tooling equipment are more. Therefore, how to realize the simple, convenient, safe and reliable release of the high-altitude balloon has important significance for balloon flight tasks.
The technical scheme of the air ball dispensing mainly comprises dynamic dispensing/static dispensing/soft dispensing/motor-driven winch dispensing/atypical wind-shield wall dispensing and the like, and specific schemes of various dispensing methods can be seen in patent CN1562702A, CN104890851A, CN107585285A, and the dispensing methods can meet the dispensing operation of various high-altitude air balls to a certain extent. The dynamic dispensing mode is mainly suitable for large heavy-duty high-altitude balloons, the static dispensing mode and atypical wind-shielding wall dispensing are suitable for medium-and small-sized high-altitude balloons, and the winch dispensing and the soft dispensing are both suitable. Various dispensing modes have certain limitations and disadvantages in view of reliability, economy and environmental suitability.
The disadvantages of various high air ball dispensing modes are as follows:
the dynamic release mode is suitable for large-scale high-altitude balloons, needs a special crane and a larger release site, and is easily influenced by weather;
the static release mode is that the nacelle and the balloon can be subjected to larger impact and vibration at the moment of towing and rising of the balloon, and are easily affected by weather;
the soft dispensing mode is characterized in that at the moment of balloon detachment, the balloon and the nacelle are not on the same vertical line, so that the nacelle can swing greatly and is subjected to larger impact and vibration, the cost of auxiliary balloons and helium used is increased, and the balloon is easily affected by weather;
the motor-driven winch is not strong in environmental adaptability in the release mode, and release operation cannot be performed when the wind load of the field is large;
the atypical in-wall dispensing device is suitable for the serial middle-small balloon dispensing, but the system is complex and the device cost is high.
In addition, the dynamic dispensing/static dispensing/soft dispensing modes have the defects of site guarantee, high number of operators and long preparation period.
Accordingly, it is desirable to provide a new high-altitude balloon dispensing apparatus and dispensing method that solve the above problems.
Disclosure of Invention
The invention aims to provide a high-altitude balloon issuing device and a high-altitude balloon issuing method, which are simple and convenient to operate, low in cost, capable of avoiding severe weather environment in a short time when in issuing preparation, and capable of fully utilizing an issuing window to achieve rapid issuing.
The technical scheme of the invention is as follows: the utility model provides a high-altitude balloon's dispensing device includes the flat-bed trolley, a plurality of being used for that the border of flat-bed trolley periphery sets up pull and dispense the high-altitude balloon's dispensing component, a plurality of dispensing component can follow the flat-bed trolley horizontal rotation and flexible action, and a plurality of dispensing component realizes dispensing action simultaneously.
In the scheme, the traction in multiple directions of the high-altitude balloon is realized through the multiple dispensing assemblies capable of horizontally rotating and stretching, and the traction position can be adjusted to be in a proper state. When the traction is released, the medium-sized, small-sized and high-altitude balloon with different sizes can be smoothly, quickly and conveniently released, and the severe weather environment can be avoided in a short time when the balloon is released.
Preferably, the dispensing assembly includes:
the rotating shaft of the rotating bracket is vertically hinged to the flat trolley;
the folding support arm is connected with the rotary support and horizontally rotates with the flat trolley through the rotary support;
the driving source drives the folding support arm to horizontally extend and retract;
and the wire stripper is arranged on the folding support arm and is used for drawing and distributing the high-altitude balloon.
The rotary support is used for realizing rotation, the folding support arm is used for realizing expansion and contraction, and the two components are combined to optimally adjust the position state before the high-altitude balloon is released.
Preferably, the wire stripper includes:
one end of the base is fixed with the upper end of the folding support arm;
the fixed end of the electric push rod is fixedly connected with the base;
the limiting pin shaft is arranged at the movable end of the electric push rod and stretches out and draws back synchronously with the movable end;
the locking block is arranged beside the electric push rod, and the limiting pin shaft is movably inserted into the locking block;
the rotating pin shaft is arranged on the base and is perpendicular to the limiting pin shaft, and the rotating pin shaft is in butt locking in the locking block through the limiting pin shaft;
and the electric push rods of the plurality of dispensing assemblies synchronously act.
According to the scheme, automatic release is realized through the extension and retraction of the electric push rod, and synchronous release actions can be better realized.
Preferably, the dispensing assembly further comprises a horizontally telescopic limiting block arranged on the flat trolley, and the limiting block is abutted and locked with the slewing bracket when being stretched.
The position of the slewing bracket is locked through the limiting block, so that the normal release is not influenced due to the fact that the position deviation is not generated before the high-altitude balloon is released.
Preferably, the folding support arm is a scissor type telescopic arm; the driving source and the wire stripper are powered by an external power supply.
The scissor type telescopic arm structure is a universal structure, the structural design and the processing are easier to realize, the design difficulty and the processing difficulty are simplified, and the cost is reduced.
Preferably, the driving source comprises a hydraulic pump, a hydraulic cylinder, a liquid storage tank and hydraulic oil, wherein a hydraulic rod of the hydraulic cylinder is connected with the folding support arm, and the hydraulic oil in the liquid storage tank is driven to the hydraulic cylinder or returns to the liquid storage tank from the hydraulic cylinder so as to realize the telescopic action of the hydraulic rod and the folding support arm.
Preferably, the head of the flat trolley is provided with a traction hook.
The present invention also provides a method for delivering a high-altitude balloon, comprising the steps of:
providing a high-altitude balloon, wherein a hanging cable is arranged at the lower end of the middle part of the high-altitude balloon, a nacelle is arranged at the tail end of the hanging cable, and a plurality of rope buckles for installing mooring cables are arranged on the outer diameter wall of the high-altitude balloon;
step two, a preparation stage before inflation:
step 2.1, deploying the dispensing device from a boat warehouse to a dispensing site through a tractor, adjusting a rotary support to a preset position, and fixing through a limiting block;
step 2.2, arranging an external power supply, and starting a driving source to unfold the folding support arm;
step 2.3, laying the high-altitude balloon at a position with a certain distance from the flat trolley, and placing the nacelle at the middle position of the flat trolley 1 while laying the high-altitude balloon;
step three, an inflation stage:
step 3.1, connecting one end of a mooring rope with the rope buckle, and knotting and connecting the other end of the mooring rope with a rotating pin shaft of the wire stripper, and simultaneously installing a high-altitude balloon;
step 3.2, detecting and confirming that the nacelle and the mooring rope are not interfered, and the suspension rope and the mooring rope are not wound;
step 3.3, filling helium into the high-altitude balloon;
step 3.4, after the inflation is completed, ensuring that each stay rope is in a tensioning state, and suspending the nacelle from the flat trolley by a distance of more than 20cm;
step four, a release stage: controlling the electric push rods in the plurality of distributing assemblies to synchronously work, pushing the limiting pin shafts to be separated from the locking blocks simultaneously, releasing the constraint of the rotating pin shafts, sliding the mooring ropes to be separated from the rotating pin shafts rapidly, and lifting the high-altitude balloon with the nacelle
Step five, completing the release operation of the high-altitude balloon; and starting the driving source to shrink the folding support arm to return to the flat trolley, and then supporting and transporting the dispensing device back to the boat warehouse through the tractor.
Preferably, the ground wind speed of the distributing site in the second step is not more than 5m/s, if the ground wind speed before distributing exceeds 5m/s, the second step and the third step are carried out in the boat warehouse, and when the ground wind speed of the distributing site is lower than 5m/s, the high-altitude balloon on the flat trolley is transported to the distributing site by the tractor to carry out distributing operation.
Preferably, before the first step, the length of the mooring rope is calculated in advance according to the helium filling volume of the ground, the height of the suspension rope, the geometric parameters of the flat trolley and the relevant parameters of the position information of the folding support arm, and the calculated length is actually 1.2 times.
Compared with the related art, the invention has the beneficial effects that: compared with a dynamic/static/soft dispensing scheme, the dispensing process is high in automation degree, the number of required dispensing personnel is small, the dispensing window is good in selection flexibility, and quick dispensing can be realized once meteorological conditions are met (the ground wind speed is lower than 5 m/s); compared with an automatic dispensing device of Google corporation in America, the invention has simple design and low cost, and can also realize the rapid dispensing of small and medium sized high-altitude balloons in function; compared with the motor-driven winch distribution scheme, the convenient distribution device can reduce the influence of meteorological conditions, can perform inflation operation in a ship warehouse, and can be immediately discharged for distribution when weather is good.
Drawings
FIG. 1 is a schematic view of a high-altitude balloon dispensing device according to the present invention;
FIG. 2 is a schematic view of the folding arm of FIG. 1;
FIG. 3 is a schematic view of the wire stripper of FIG. 1;
FIG. 4 is a schematic illustration of a dispensing device, a pre-inflation preparation stage of a dispensing balloon;
FIG. 5 is a schematic illustration of the dispensing apparatus, dispensing balloon, and the stage of inflation preparation;
fig. 6 is a schematic view of the lift-off phase of the dispensing device dispensing a balloon.
In the drawings, a 1-flat trolley, a 2-folding support arm, a 3-wire stripper, a 4-hydraulic component, a 5-rotary support, a 6-limiting block, a 7-hydraulic rod, an 8-mooring cable, a 9-inner hinge frame, a 10-electric push rod, an 11-limiting pin shaft, a 12-rotating pin shaft, a 13-base, a 14-boat warehouse, a 15-high-altitude balloon, a 16-nacelle, a 17-hanging cable, an 18-traction hook, a 19-locking block and a 20-support.
Detailed Description
The invention will be described in detail below with reference to the drawings in connection with embodiments. It should be noted that, without conflict, the embodiments of the present invention and features of the embodiments may be combined with each other. For convenience of description, the words "upper", "lower", "left" and "right" are used hereinafter to denote only the directions corresponding to the upper, lower, left, and right directions of the drawings, and do not limit the structure.
As shown in fig. 1 to 3, the high-altitude balloon dispensing device provided in this embodiment includes a flat-panel trolley 1, and a plurality of dispensing assemblies for drawing and dispensing the high-altitude balloon, which are disposed at the edges of the periphery of the flat-panel trolley 1, wherein the plurality of dispensing assemblies can horizontally rotate and stretch along the flat-panel trolley 1, and the plurality of dispensing assemblies simultaneously realize the dispensing operation.
The flat trolley 1 is refitted on a traction type flat trailer, the length, width and height of the flat trailer are 6m multiplied by 2.5m multiplied by 0.6m, and the front wheel of the flat trolley 1 is connected with a trolley bottom bearing so that the trolley has turning capability. The weight of the flat trolley 1 is more than 200kg, and sandbags or other heavy objects can be placed on the trolley platform for counterweight when the dead weight is insufficient. The flat trolley 1 is a non-standard customized steel flat trailer, and a locomotive head is provided with a traction hook 18 for connecting the traction vehicle to carry out transportation and transfer operation of the dispensing device.
The four dispensing assemblies are respectively arranged at four end corners of the flat trolley 1. The dispensing assembly comprises a rotary support 5, a folding support arm 2, a driving source 4, a wire stripper 3 and a limiting block 6, wherein a rotating shaft of the rotary support 5 is vertically hinged to the flat trolley 1. The slewing bracket 5 comprises an external tooth slewing bearing turntable bearing 21, a mounting frame 22 and a bolt assembly (not shown), wherein the mounting frame 22 is mounted on the external tooth slewing bearing turntable bearing 21 through bolts, and the folding support arm 2 is connected with the mounting frame 22, so that the folding support arm can horizontally rotate. The horizontal rotation means that the rotation direction is parallel to the ground. The structure of the slewing bearing 5 is the same as that of the existing slewing bearing which is mature in the market. The length and width distances of the rotary brackets 5 from the end angle of the flat trolley 1 are consistent, and the rotary brackets are fixedly connected with the flat trolley 1 through screws, so that the rotary brackets can freely rotate in a plane without barriers.
The folding support arm 2 is connected with the revolving support 5, and horizontally rotates with the flat trolley 1 through the revolving support 5. The folding support arm 2 is a scissor type telescopic arm formed by the head-to-tail staggered hinging of a plurality of inner hinge frames of aluminum profiles. The diamond shape is contracted when in use. The driving source 4 and the wire stripper 3 are powered by a 24V external power supply. When the hydraulic rod 7 of the driving source 4 is extended, the inner hinge frame at one side of the scissor fork is driven to extend, so that the whole extension of the folding support arm 2 is realized. And conversely, the device is retracted. The fully unfolded or contracted time of the folding support arm 2 is not more than 5min, the fully contracted length is not more than 1.5m, the folding support arm can be placed on a trolley plane, and when the driving source 4 fails, the folding support arm can be stretched by personnel. The horizontal extension and retraction realized by the folding support arm 2 refers to extension and retraction along the direction parallel to the ground of the flat trolley 1.
The driving source 4 drives the folding support arm 2 to horizontally extend and retract. The thread stripper 3 is arranged on the folding support arm 2 and is used for drawing and distributing the high-altitude balloon.
The driving source 4 comprises a hydraulic pump, a hydraulic cylinder, a liquid storage tank and hydraulic oil, a hydraulic rod 7 of the hydraulic cylinder is connected with the folding support arm 2, and the hydraulic oil in the liquid storage tank is driven to the hydraulic cylinder or returns to the liquid storage tank from the hydraulic cylinder so as to realize the telescopic action of the hydraulic rod 7 and the folding support arm 2.
The thread stripper 3 is arranged on an inner hinge frame 9 of the folding support arm 2, and in order to realize the release of balloons with different volumes, thread connecting holes are reserved in the middle of the inner hinge frame 9 of each telescopic unit for arranging the thread stripper 3. The wire stripper 3 comprises a base 13, an electric push rod 10, a limiting pin 11, a locking block 19 and a rotating pin 12, wherein the base 13 is of a rectangular plate-shaped structure, the length edge of one end of the base is fixed with the upper end of one inner hinge frame 9 of the folding support arm 2, and the other end of the base is not connected, so that the wire stripper 3 does not interfere the telescopic action of the inner hinge frame 9.
The electric push rod 10 is a miniature linear electric push rod of the current mature product, the miniature linear electric push rod is arranged along the length direction of the base 13, the fixed end of the miniature linear electric push rod is fixedly connected with the base 13, and the output end of the miniature linear electric push rod is provided with the limiting pin shaft 11. The locking piece 19 is arranged at the side of the electric push rod 10. The locking blocks 19 are supporting plate structures arranged at intervals, and holes for the limiting pin shafts 11 to pass through are formed in the upper ends of the supporting plate structures.
The rotating pin shaft 12 is vertically arranged on the base 13 and is perpendicular to the limiting pin shaft 11, that is, one end of the rotating pin shaft 12 is hinged to the base 13, the other end of the rotating pin shaft is inserted into two support plates of the locking block 19, and the two support plates are locked in an abutting mode through the limiting pin shaft 11. When the output end of the electric push rod 10 stretches, the limiting pin shaft 11 is driven to stretch simultaneously, and when the limiting pin shaft 11 stretches to be separated from the support plate of the locking block 19, the rotating pin shaft 12 is released and locked. At the moment of release, the electric push rods 10 of the four release assemblies synchronously act to realize synchronous release of the high-altitude balloon.
The rotating pin shaft 12 is connected with a mooring cable of the high-altitude balloon, and the rotating action of the rotating pin shaft is limited by the limiting pin shaft 11. When the electric push rod 10 is powered on and pushes the limiting pin shaft to move, the rotating pin shaft 12 immediately acts to promote the mooring rope 8 to be separated from the wire stripper 3.
The limiting block 6 is a metal part, the extending tail end of the limiting block is triangular, the main body is fixed on the flat trolley 1 through an n-shaped bracket 20 through bolts, the triangular extending tail end of the limiting block points to an external tooth slewing bearing turntable bearing 21 of the slewing bracket 5, and bolts for locking the position of the limiting block 6 through adjustment are arranged in the middle of the bracket 20. When the locking is needed, the limiting block 6 is pushed to the direction of the slewing bracket 5, so that the triangle at the tail end of the limiting block 6 is externally meshed with the external tooth slewing bearing turntable bearing 21 to fix the position of the limiting block, and otherwise, the locking is released.
In another embodiment, the number of the limiting blocks 6 is two, and the limiting blocks are distributed at two ends of the diameter of the external tooth slewing bearing turntable bearing 21 so as to realize two-phase-to-point locking.
The design parameters of the high air ball system of the selected example are as follows:
(1) Balloon type: unitary pumpkin-shaped overpressure balloon.
(2) System weight parameters:
the weight of the air bag is as follows: 60.4kg;
load pod structural weight: 12kg;
computer, energy, parachute, valve and other electromechanical equipment weight: 70kg.
(3) Design geometry parameters
Balloon diameter: 17.0m (after design dwell height expansion molding);
free rib length: 22.3m;
pod height: 0.77m;
suspension cable height between pod and balloon: 15m.
(4) Other parameters
Helium filling volume on the ground: 165.6m 3
Ground net buoyancy: 25.05kg;
designing the height of the residence: 20km.
As shown in fig. 1 to 6, the present invention provides a method for delivering a high-altitude balloon, comprising the following steps:
s1, calculating length data of the mooring rope 8 in advance according to the helium filled volume on the ground, the height of the suspension rope 17, geometric parameters of the trolley, position information of the folding support arm 2 and the like, taking 1.2 times of the calculated length of the rope, and calculating to obtain the length of the mooring rope 8 which is about 22.2m. In the dispensing process, if the length of the cable is too long or too short, the cable can be replaced in real time.
S2, providing a high-altitude balloon 15, wherein a hanging cable 17 is arranged at the lower end of the middle part of the high-altitude balloon 15, a nacelle 16 is arranged at the tail end of the hanging cable 17, and a plurality of rope buckles for installing the mooring ropes 8 are arranged on the outer diameter wall of the high-altitude balloon 15.
S3, preparation stage before inflation:
s3.1, if the ground wind speed of the issuing site is not more than 5m/S, deploying the issuing device from the boat warehouse 14 to the issuing site through a tractor, adjusting the slewing bracket 5 to a preset position, and fixing through the limiting block 6;
s3.2, an external 24V power supply is arranged, and a driving source 4 is started to unfold a folding support arm 2;
and S3.3, paving the high-altitude balloon 15 at a position 2m away from the trolley, and placing the nacelle 16 at the middle position of the trolley 1 at the same time of paving. When all the arrangement work is completed, the device debugging before the release of the high-altitude balloon 15 is performed.
S4, an inflation stage:
s4.1, fully expanding the folding support arm 2 at a preset position, connecting one end of the mooring rope 8 with the rope buckle, and tying the other end of the mooring rope into a circular ring (which can be in a winding form and can be automatically unwound by buoyancy of a high-altitude balloon), connecting the circular ring with the rotating pin shaft 12 of the wire stripper 3, and simultaneously installing the high-altitude balloon 15 (such as connection among a parachute, a nacelle and an unlocking device);
s4.2, detecting and confirming that the pod 16 and the mooring rope 8 are not interfered with each other, and that the suspension rope 17 and the mooring rope 8 are not wound;
s4.3 by three helium packaging grids (40 m total 3 Not shown) helium is supplied to the high-altitude balloon 15;
s4.4, after inflation is completed, each tethered cable 8 is ensured to be in a tensioning state, and the nacelle 16 is suspended at a distance of more than 20cm from the flat trolley 1, so that impact and vibration caused by dragging the nacelle 16 by the instant balloon 15 are avoided. The slewing bracket 5 is locked by a limiting block 6.
S5, a release phase: if the real-time ground wind speed is not more than 5m/s and the weather is good, the electric push rods in the plurality of distributing assemblies are controlled to work synchronously, meanwhile, the limiting pin shafts 11 are pushed to be separated from the locking blocks 19, the constraint of the rotating pin shafts 12 is released, the mooring ropes 8 slide to be separated from the rotating pin shafts 12 rapidly, and the high-altitude balloon 15 is lifted off with the nacelle 16. In the dispensing process, the four electric push rods 10 act uniformly
S6, completing the release operation of the high-altitude balloon; the driving source 4 is started to retract the folding support arm 2 to return to the flat trolley 1, and then the delivery device is supported and transported back to the boat warehouse 14 through the tractor.
If the ground wind speed before the release exceeds 5m/S, a series of preparation works before the release in the steps S3 and S4 can be carried out in the boat warehouse, and when the ground wind speed is lower than 5m/S, the balloon 15 on the flat trolley 1 is hauled to the release site by the tractor to carry out release operation. In addition, if the ground wind speed is high when the air bag is ready to be released, the air bag 15 can be transported to the boat warehouse through the tractor, and the releasing operation is performed after the weather is changed, but the problem of leakage of the air bag skin material is considered, and the time for the air bag 15 to stay in the boat warehouse 14 is not suitable to exceed 1 day.
The dispensing device adjusts the plane position of the folding support arm 2 through the rotary support 5, and adjusts the position of the thread stripper 3 on the folding support arm 2, and the constraint between the mooring rope 8 and the dispensing device is relieved by means of simultaneous actions of four electric push rods 10, so that smooth dispensing of medium-sized and small-sized high-altitude air balls with different sizes is realized.
In another embodiment, the rotation pin can exit the release balloon, and can be realized by any one of tripping, exiting and cutting functions.
The foregoing description is only illustrative of the present invention and is not intended to limit the scope of the invention, and all equivalent structures or equivalent processes or direct or indirect application in other related technical fields are included in the scope of the present invention.

Claims (9)

1. The high-altitude balloon dispensing device is characterized by comprising a flat trolley (1) and a plurality of dispensing components which are arranged at the edge of the periphery of the flat trolley (1) and used for drawing and dispensing the high-altitude balloon, wherein the dispensing components can horizontally rotate and stretch along the flat trolley (1) and simultaneously realize dispensing;
the rotating shaft of the rotating bracket (5) is vertically hinged to the flat trolley (1);
the folding support arm (2) is connected with the rotary support (5) and horizontally rotates with the flat trolley (1) through the rotary support (5);
the driving source (4) drives the folding support arm (2) to horizontally extend and retract;
the wire stripper (3) is arranged on the folding support arm (2) and is used for drawing and distributing a high-altitude balloon;
the folding support arm (2) is a scissor type telescopic arm formed by head-to-tail staggered hinging of a plurality of inner hinges (9); the wire stripper (3) is arranged on an inner hinge bracket (9) of the folding support arm (2), and threaded connection holes are reserved in the middle of the inner hinge bracket (9) of each telescopic unit and used for arranging the wire stripper (3).
2. A high-altitude balloon issuing apparatus according to claim 1, wherein said doffer (3) comprises:
a base (13) one end of which is fixed with the upper end of the folding support arm (2);
the fixed end of the electric push rod (10) is fixedly connected with the base (13);
the limiting pin shaft (11) is arranged at the output end of the electric push rod (10) and stretches out and draws back synchronously with the output end;
the locking block (19) is arranged beside the electric push rod (10), and the limiting pin shaft (11) is movably inserted into the locking block (19);
the rotating pin shaft (12) is arranged on the base (13) and is perpendicular to the limiting pin shaft (11), and the rotating pin shaft (12) is in butt locking in the locking block (19) through the limiting pin shaft (11);
and the electric push rods (10) of the plurality of the dispensing assemblies synchronously act.
3. The high-altitude balloon dispensing device according to claim 1, wherein the dispensing assembly further comprises a horizontally retractable stopper (6) provided on the flatcar (1), the stopper (6) being locked in abutment with the slewing bracket (5) when extended.
4. The high-altitude balloon dispensing device according to claim 1, wherein the driving source (4) and the wire stripper (3) are powered by an external power source.
5. The high-altitude balloon dispensing device according to claim 1, wherein the driving source (4) comprises a hydraulic pump, a hydraulic cylinder, a liquid storage tank and hydraulic oil, the hydraulic rod (7) of the hydraulic cylinder is connected with the folding support arm (2), and the hydraulic oil in the liquid storage tank is driven to the hydraulic cylinder or returned to the liquid storage tank from the hydraulic cylinder so as to realize the telescopic action of the hydraulic rod (7) and the folding support arm (2).
6. A device for dispensing high-altitude balloons according to claim 1, characterized in that the head of the trolley (1) is provided with a traction hook (18).
7. A method for delivering a high-altitude balloon, comprising the steps of:
step one, providing a high-altitude balloon (15), wherein a hanging cable (17) is arranged at the lower end of the middle part of the high-altitude balloon (15), a nacelle (16) is arranged at the tail end of the hanging cable (17), and a plurality of rope buckles for installing mooring ropes (8) are arranged on the outer diameter wall of the high-altitude balloon (15);
step two, a preparation stage before inflation:
step 2.1, deploying the dispensing device according to any one of claims 3-6 from a boat warehouse (14) to a dispensing site through a tractor, adjusting a slewing bracket (5) to a preset position, and fixing through a limiting block (6);
step 2.2, arranging an external power supply, and starting a driving source (4) to unfold the folding support arm (2);
step 2.3, laying a high-altitude balloon (15) at a position with a certain distance from the flat trolley (1), and placing a nacelle (16) at the middle position of the flat trolley 1 while laying;
step three, an inflation stage:
step 3.1, fully unfolding the folding support arm (2) at a preset position, connecting one end of a mooring rope (8) with the rope buckle, knotting and connecting the other end of the mooring rope with a rotary pin shaft (12) of the wire stripper (3), and simultaneously installing a high-altitude balloon (15);
step 3.2, detecting and confirming that there is no interference between the nacelle (16) and the mooring line (8), and that the suspension line (17) and the mooring line (8) are not wound;
step 3.3, filling helium into the high-altitude balloon (15);
step 3.4, after the inflation is completed, ensuring that each stay rope (8) is in a tensioning state, and suspending the nacelle (16) from the flat trolley (1) by a distance of more than 20cm;
step four, a release stage: the electric push rods in the plurality of dispensing assemblies are controlled to synchronously work, meanwhile, the limiting pin shafts (11) are pushed to be separated from the locking blocks (19), the constraint of the rotating pin shafts (12) is released, the mooring ropes (8) slide to be separated from the rotating pin shafts (12) rapidly, and the high-altitude balloon (15) is lifted off with the nacelle (16);
step five, completing the release operation of the high-altitude balloon; the driving source (4) is started to shrink the folding support arm (2) to return to the flat trolley (1), and then the distributing device is supported and transported back to the boat warehouse (14) through the tractor.
8. The method for delivering high-altitude balloon according to claim 7, wherein the ground wind speed of the delivering site in the second step is not more than 5m/s, and if the ground wind speed before delivering exceeds 5m/s, the second step and the third step are performed in the boat warehouse (14), and when the ground wind speed of the delivering site is lower than 5m/s, the high-altitude balloon (15) on the tractor-hauling flat-bed trolley (1) is delivered to the delivering site for delivering operation.
9. The method according to claim 7, wherein the length of the mooring rope (8) is calculated in advance before the first step according to the ground helium filling volume, the height of the suspension rope (17), the geometric parameters of the flat trolley (1) and the position information related parameters of the folding support arm (2), and the calculated length is actually 1.2 times.
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Publication number Priority date Publication date Assignee Title
CN111824383B (en) * 2020-06-15 2021-12-21 中国科学院空天信息创新研究院 Synchronous release mechanism and high-altitude balloon restraint device
CN111874206A (en) * 2020-08-17 2020-11-03 哈尔滨工业大学(深圳) Cut fork telescoping device and applied this unmanned aerial vehicle who cuts fork telescoping device

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4402479A (en) * 1981-06-19 1983-09-06 Westinghouse Electric Corp. Small tethered aerostat relocatable system
CN1562702A (en) * 2004-03-17 2005-01-12 中国科学院高能物理研究所 Method for putting out high-altitude balloon
CN101898633A (en) * 2010-04-28 2010-12-01 湖南航天管理局 All-in-one anchoring trailer
CN103612741A (en) * 2013-12-16 2014-03-05 江苏科技大学 Engine driven type captive balloon lift-off recovery system
CN104890851A (en) * 2015-05-25 2015-09-09 湖南航天机电设备与特种材料研究所 Near space balloon system safety release method
CN106516069A (en) * 2016-10-25 2017-03-22 中国电子科技集团公司第三十八研究所 Mobile anchoring vehicle for withdrawing, releasing and parking of tethered balloon
CN108163179A (en) * 2017-12-06 2018-06-15 湖南航天远望科技有限公司 A kind of near space aerostatics distribution method and dispensing apparatus
CN208377039U (en) * 2018-06-15 2019-01-15 湖南航天远望科技有限公司 A kind of captive balloon sphere, shelter for guaranteeing and its captive balloon system

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4402479A (en) * 1981-06-19 1983-09-06 Westinghouse Electric Corp. Small tethered aerostat relocatable system
CN1562702A (en) * 2004-03-17 2005-01-12 中国科学院高能物理研究所 Method for putting out high-altitude balloon
CN101898633A (en) * 2010-04-28 2010-12-01 湖南航天管理局 All-in-one anchoring trailer
CN103612741A (en) * 2013-12-16 2014-03-05 江苏科技大学 Engine driven type captive balloon lift-off recovery system
CN104890851A (en) * 2015-05-25 2015-09-09 湖南航天机电设备与特种材料研究所 Near space balloon system safety release method
CN106516069A (en) * 2016-10-25 2017-03-22 中国电子科技集团公司第三十八研究所 Mobile anchoring vehicle for withdrawing, releasing and parking of tethered balloon
CN108163179A (en) * 2017-12-06 2018-06-15 湖南航天远望科技有限公司 A kind of near space aerostatics distribution method and dispensing apparatus
CN208377039U (en) * 2018-06-15 2019-01-15 湖南航天远望科技有限公司 A kind of captive balloon sphere, shelter for guaranteeing and its captive balloon system

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